Airbus A300-600 vs. North American B-25 Mitchell

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Airbus A300-600 versus North American B-25 Mitchell
54.10 m 177 ft 6 in length 16.15 m 53 ft 0 in
16.5 m 54 ft 2 in height 5 m 16 ft 4 in
44.84 m 147 ft 1 in wingspan 20.58 m 67 ft 6 in
2 x turbofan engines, either Pratt & Whitney PW 4000 or General Electric GE CF6-80C2A1 engines 2 x Wright R-2600-92 Twin Cyclone
56,000lb to 61,500lb thrust per engine 1,700 horsepower
112,000–123,000 lb total thrust 3,400 horsepower
171,700 kg 378,600 lb MTOW 7,484 kg 16,500 lb
7,500 km 4,052 nm range 1,350 mi 1,175 nm
897 km/h 557 mph cruise speed 233 MPH 375 km/h
210-250 passengers capacity
rotor diameter
rate of climb
Please note that these values are indicative and actual values can vary based on specific engine models and configurations.